View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68437U 26145.12642978 +.00000000 +00000-0 +64559-3 0 00000
2 68437 97.4490 103.9262 0004767 108.4183 251.7570 15.18932262 01
| Epoch (UTC): | 25 May 2026 03:02:03 |
| Eccentricity: | 0.0004767 |
| inclination: | 97.4490° |
| perigee height: | 506 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 103.9262° |
| argument of perigee: | 108.4183° |
| revolutions per day: | 15.18932262 |
| mean anomaly at epoch: | 251.7570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|